Actuation Mechanism And Associated Methods

ABSTRACT

An actuation mechanism used in, for example, a missile assembly is disclosed, as are methods of its use. The actuation mechanism is locked in a first orientation and is unlocked in a second orientation. Locking and unlocking of the actuation mechanism is achieved by way of a locking mechanism that responds to a certain stimulus. In some embodiments, the actuation mechanism is incorporated into a sub-assembly of a missile to assist in controlling the missile&#39;s flight.

BACKGROUND OF THE INVENTION

This application is a divisional of U.S. application Ser. No.15/004,228, filed on Jan. 22, 2016, the disclosure of which isincorporated herein by reference.

The present invention relates to an actuation mechanism and associatedmethods of use, for example in military applications.

Certain military devices (and devices in other industries) requireactuation mechanisms that are fast-acting and responsive in a reliablemanner. As an example, missile technologies use actuation mechanismsthat lock or unlock the missile's flight controls. Frequently, theseactuation mechanisms are a “single use” device. In other words, aftertriggering the actuation mechanism, it is no longer usable. In this way,it can be difficult to test or validate certain actuation mechanisms forfield operation. Other downfalls of common actuation mechanisms are alsopresent.

It is therefore an object of the present invention to provide anactuation mechanism and associated systems and methods that improve uponexisting devices.

BRIEF SUMMARY OF THE INVENTION

A first aspect of the invention includes an actuation mechanismcomprising a housing having an internal hollow bore. A plunger ismovably positioned inside the hollow bore of the housing, and a lockingmechanism is movable between a first position configured to lock theplunger relative to the housing and a second position configured tounlock the plunger relative to the housing. The actuation mechanism alsocomprises a piston having a body and a wire engaged to the piston andthe plunger, the wire being composed of a material configured to changeits length in response to a stimulus, wherein when the wire is subjectedto the stimulus, the wire changes its length and moves the piston from afirst position to a second position, which causes the locking mechanismto move from its first position to its second position and unlock theplunger relative to the housing.

In embodiments of this first aspect, the wire is composed of a materialselected from the group consisting of a shape-memory alloy and anickel-titanium shape memory alloy.

A second aspect of the invention includes a method of operating anactuation mechanism comprising: (1) positioning a plunger inside a borein a housing, such that the plunger is locked relative to the housing,(2) fixedly engaging a wire to a piston and to the plunger, and (3)subjecting the wire to a stimulus so that the wire changes its lengthand causes the piston to move from a first position to a secondposition, the movement of the piston from the first position to thesecond position serving to unlock the plunger relative to the housing sothat the plunger is free to move inside the bore relative to thehousing. Although numbered steps are provided above, it is to beunderstood that no particular order of steps is required for the method.

In embodiments of the second aspect, the stimulus is an electriccurrent, a temperature stimulus, or a combination thereof. In addition,the piston may have at least one internal channel with the wireextending through the at least one internal channel.

BRIEF DESCRIPTION OF THE DRAWINGS

A more complete appreciation of the subject matter of the presentinvention and of the various advantages thereof can be realized byreference to the following detailed description in which reference ismade to the accompanying drawings in which:

FIGS. 1A-B are cross-sectional views of an actuation mechanism, shown inlocked and unlocked positions.

FIG. 2 is a perspective view of an exemplary missile sub-assembly inwhich the actuation mechanism of FIGS. 1A-B can be used.

FIGS. 3A-B are cross-sectional views of the sub-assembly of FIG. 2,showing an alternate embodiment of the actuation mechanism of FIGS. 1A-Bin locked and unlocked positions.

FIG. 4 is a perspective view of the output shaft forming part of thesub-assembly of FIGS. 2-3B.

DETAILED DESCRIPTION

In describing certain aspects of the present invention, specificterminology will be used for the sake of clarity. However, the inventionis not intended to be limited to any specific terms used herein, and itis to be understood that each specific term includes all technicalequivalents, which operate in a similar manner to accomplish a similarpurpose.

FIGS. 1A-B are cross-sectional views of an actuation mechanism 10 usedin, for example, military applications. In a particular embodiment,actuation mechanism 10 is used in a sub-assembly of a missile system, asshown in more detail in FIGS. 2 and 3A-B. Actuation mechanism 10 can beused to trigger or allow operation of a control assembly in the missilefor controlling the missile's flight mechanisms (e.g., its fins). Otherapplications for actuation mechanism 10 are, of course, possible asdescribed in more detail below.

Referring to FIGS. 1A-B, actuation mechanism 10 includes a fixed housing20 that, in an embodiment, has an outer threaded area 22 for connectionwith another structure. Alternative connection mechanisms besidesthreading may also be used (e.g., press-fit, bayoneted connection,welding, etc.). In addition, as shown in FIGS. 2 and 3A-B, fixed housing20 is in an alternate embodiment incorporated or monolithic with anotherstructure, such as a portion of a missile sub-assembly. Fixed housing 20includes a hollow shaft 26 and a groove 24 positioned between shaft 26and threaded area 22 for receiving a spring 27 or other flexible member(e.g., a flexible disc).

Hollow shaft 26 of fixed housing 20 has a length that is greater thanthat of threaded area 22, such that shaft 26 extends outwards fromthreaded area 22. Hollow shaft 26 is a cylindrical shaft, in anembodiment, with a hollow inside to house additional components ofactuation mechanism 10. As an example, a plunger 40 and piston 70mechanism can be positioned inside of hollow shaft 26, as illustrated inFIGS. 1A-B.

Inside of hollow shaft 26 is a plunger 40 that is movable relative toshaft 26. Thus, the diameter of hollow shaft 26 is only slightly largerthan the diameter of plunger 40 so that plunger 40 can fit within hollowshaft 26 in a movable relationship. In other words, the diameters ofhollow shaft 26 and plunger 40 are such that plunger 40 can fit tightlywithin hollow shaft 26, yet still slide along the inside of shaft 26 ineither direction. In an exemplary embodiment, the diameter of hollowshaft 26 is 260 mm while the diameter of plunger 40 is 259 mm.

As shown in FIGS. 1A-B, plunger 40 has a flange 42 at a first end, and apartly hollow shaft 44 extending from flange 42. At a second end,plunger 40 has a reset mechanism 58, which in an embodiment is athreaded bore. An internal cavity 46 extends into plunger 40 adjacentflange 42 for housing piston 70. Internal cavity 46 is a stepped cavity,in an embodiment, which has a larger diameter section 48 and a smallerdiameter section 50 between which a step is located. Smaller diametersection 50 of internal cavity 46 houses a fixed member 52 (e.g., a fixedcylindrical post), while larger diameter section 48 houses a piston 70and spring 54 mechanism. Larger diameter section 48 may also includemultiple openings 60 for receiving balls 56, which form a part of alocking mechanism as described below. Although multiple openings 60 andballs 56 are shown, it is equally contemplated that a single opening 60and ball 56 could be used, or more than two (2) openings 60 and balls 56could be used. Openings 60 and balls 56 work in conjunction with one ormore recesses or grooves 28 of fixed housing 20 to lock housing 20relative to plunger 40, as set forth in detail below. In some instances,a single groove 28 extends circumferentially about the inside of shaft26 of fixed housing 20, although in other cases a simple recess orrecesses 28 formed along only part of the inside of shaft 26 could alsobe used. As an example, multiple recesses 28 may be provided, with onerecess 28 being available for each ball 56 and having adimension/geometry configured to retain the relevant ball 56. In aparticular embodiment, each recess 28 may have a taperedgeometry/section for reasons described below.

Piston 70 is also shown in FIGS. 1A-B. Piston 70 may be positionedinside internal cavity 46 of plunger 40 in an abutting relationship tospring 54 (e.g., a helical spring). Other springs or biasing members—forexample a flexible/compressible cylindrical post, a Bellevillewasher(s), etc.—may be used in place of spring 54, of course. Due topiston 70's position against spring 54, piston 70 can movelongitudinally within larger diameter section 48 of internal cavity 56against the force of spring 54. In an embodiment, piston 70 includes amain body 74 and a stepped shaft 76 extending from main body 74 (e.g.,two (2) steps), which includes a bushing 72 on the last step. Bushing 72may be fixedly adhered to piston 70 as by welding, gluing, or otherprocesses, and it may include a tapered section 73 set at an angle to astraight section 75. In other embodiments, bushing 72 is omitted and thegeometry of stepped shaft 76 of piston 70 is monolithically formed tomatch that of bushing 72. Bushing 72 presents a surface that facesspring 54 to contacts spring 54's coils so that spring 54 may becompressed longitudinally by way of piston 70. For instance, spring 54may be positioned between bushing 72 and the step between larger andsmaller diameter sections 48, 50 and be compressed against the step. Asan example, the distance between the step and bushing 72 may be smallerthan the uncompressed length of spring 54, placing spring 54 in acompressed state.

Piston 70 also includes internal channels 78 extending through main body74 and shaft 76 for receiving a wire 90. Wire 90 may extend throughchannels 78 and around fixed post 52, which is fixedly attached oralternatively monolithic with plunger 40. As described in more detailbelow, wire 90 may be composed of a shape-memory material or any othermaterial that changes its length (e.g., contracts) when subjected to acertain stimulus (e.g., an electric current, temperature stimulus, etc.)For instance, wire 90 is composed of nickel-titanium shape memory allow,such that wire 90 changes in length, for instance it contracts, whensubjected to an electric current. The electric current is provided by anelectricity source (e.g., a battery) coupled to wire 90. In a specificembodiment, wire 90 may decrease in length by about 2-10%, moreparticularly about 4%, when subjected to an appropriate electriccurrent. Thus, the length contraction of wire 90 may be configured sothat it generates a sufficient force to overcome the counter-biasingforce of spring 54, which is positioned in an abutting relationship topiston 70.

Channels 78 extend entirely through piston 70, in an embodiment, andalso intersect with at least one opening 80 in piston 70 for receiving aset screw 82. As shown in FIGS. 1A-B, two (2) openings 80 and two (2)set screws 82 are used, although more or less openings 80 and set screws82 can be utilized. Openings 80 open out into channels 78 so that setscrews 82 can be screwed into openings 80 and pinch wire 90 against asurface of piston 70 to fix wire 90 relative to piston 70. In otherembodiments, different structures besides set screws 82 can be used suchas, for example, a spring-actuated push button that fixes wire 90, apress-fit mechanism in openings 80 for fixing wire 90, or aquick-release mechanism for fixing wire 90.

Actuation mechanism 10 is shown in a locked position in FIG. 1A and anunlocked position in FIG. 1B. The following describes the movement ofactuation mechanism 10 from the locked to unlocked positions. In use,actuation mechanism 10 may be assembled as shown in FIGS. 1A-B—in otherwords with plunger 40 inside fixed housing 20, piston 70 and springs 27,54 in place, and wire 90 extending through internal channels 78 ofpiston 70 and around post 52. Since wire 90 is wrapped around post 52and fixed in one or more locations to piston 70 via set screws 82,contraction of wire 90 causes movement of piston 70 against spring 54 ina laterally-rightward direction when looking to FIG. 1A. Consequently,balls 56 are free to move from their initial, locked location withinrecesses 28 of fixed housing 20, to a secondary, unlocked locationagainst shaft 76 of piston 70, as shown in FIG. 1B. Due to the geometryof tapered section 73 of bushing 72 and the geometry of the taperedsection of recesses 28, balls 56 are forced inward towards shaft 76 ofpiston 70. In particular, piston 70 moves laterally right by a distancesufficient to move bushing 72 beyond the extent of recesses 28, therebyproviding space for balls 76 to move inward. Since balls 56 are incontact with openings 60 of plunger 40, and spring 27 is constantlybiased to move plunger 40 laterally left, plunger 40 moves balls 56against the tapered section of recesses 28 causing balls 58 to move outof recesses 28 towards piston 70. Balls 56 therefore move from a firstorientation in which balls 56 contact both fixed housing 20 and plunger40 (e.g., via recesses 28 and openings 60, respectively) to lock housing20 and plunger 40 relative to each other, to a second orientation inwhich balls 56 move inward towards shaft 76 of piston 70 and ride alongthe inside of hollow shaft 26 of fixed housing 20. In the secondorientation, plunger 40 is unlocked and can freely translate relative tofixed housing 20.

With balls 56 in their unlocked position—caused by the contraction ofwire 90 via an external stimulus (e.g., an electric current)—actuationmechanism 10 may move to its unlocked state, as shown in FIG. 1B. Inparticular, plunger 40 may be forced in a laterally-leftward directionwhen looking at FIG. 1B by way of spring 27 acting on flange 42 ofplunger 40. In other words, since the movement of balls 56 has placedactuation mechanism 10 in an unlocked state as described above, andspring 27 is in a compressed state sandwiched between flange 42 ofplunger 40 and groove 24 of fixed housing 20 when actuation mechanism 10is in a locked state, spring 27 may act against flange 42 and causeplunger 40 to move laterally leftward, as reflected by the transitionbetween FIGS. 1A-B. This allows other assemblies associated withactuation mechanism 10 (e.g., a flight controller for a missile) tobecome unlocked as well.

To manually reset actuation mechanism 10 into its locked state (FIG.1A), wire 90 is allowed to cool and a tool (not shown) may be engagedwith reset mechanism 58. The tool is used to pull plunger against spring27 in a rightward direction relative to fixed housing 20 so that balls56 move outward back into recesses 28 and cause plunger 40 to becomelocked again relative to fixed housing 20. In this regard, in aparticular embodiment balls 56 may be biased outwards so that, asplunger 40 moves in a rightward direction relative to fixed housing 20,balls 56 automatically snap back into place within recesses 28 of fixedhousing 20 once plunger 40 is moved far enough. This is achieved by wayof piston 70 and bushing 72. For instance, balls 56 are able to snapback into recesses 28 because wire 90 has cooled and piston 70 isthereby moved back to its original location. With wire 90 cooled andallowed to expand, spring 54 constantly forces piston 70 in a leftwarddirection causing tapered section 73 of bushing 72 to force balls 56outwards. Once plunger 40 is pulled so that balls 56 align with recesses28, balls 56 will automatically snap back into place within recesses 28and lock plunger 40 relative to fixed housing 20.

As noted previously, although reset mechanism 58 is a threaded bore inone embodiment, and tool likewise includes a threaded section (notshown) for connection with reset mechanism 58, other connectionmechanisms can be used (e.g., press-fit, bayonetted connection,ball-and-detent mechanism, etc.) With actuation mechanism 10 in itslocked state, as shown in FIG. 1A, actuation mechanism 10 can be usedagain, as needed. The manual reset mechanism 58 described above is alsouseful for testing actuation mechanism 10 prior to its use.

FIGS. 2 and 3A-B depict an alternate embodiment of actuation mechanism10—actuation mechanism 10′ —in use in the context of a missilesub-assembly 130. Actuation mechanism 10′ includes the same structuresand functionality as actuation mechanism 10, unless otherwise indicated.In that regard, like numerals refer to like elements in this embodiment,except that a prime series of reference numerals is used in thealternate embodiment for like elements, while new elements are accordednew reference numerals.

Missile sub-assembly 130 is a control assembly for controlling certainflight mechanisms in a missile, for instance the missile's fin(s) (notshown). Missile sub-assembly 130 includes a mounting 122 with an opening124, and an output shaft 110 positioned in opening 124. Output shaft 110is coupled to another mechanism (not shown) for moving the fins of themissile and thereby controlling the missile's flight.

As shown in FIGS. 3A-B and 4, output shaft 110 has a hollow cylindricalbody 112 with gears or teeth 114 extending from a first side of body112, and a projection 116 extending from a second side of body 112.Additionally, within opening 124 in mounting 122 are a set of bearings120 surrounding body 112 of output shaft 110 to allow rotation of outputshaft 110 within opening 124. Gears 114 of output shaft 110 may beconnected to another gear mechanism (not shown) that is controlled by anon-board computing device or other control mechanism (not shown)designed to rotate output shaft 110 via gears 114 and control the flightof the missile by altering the position of the missile's fins. Stateddifferently, the missile may include an on-board computer or controlmechanism that, in response to measuring various environmental flightconditions of the missile, can send a signal to control a gear mechanism(not shown) engaged with gears 114, thereby causing the gear mechanism(not shown) to move gears 114 and output shaft 110. Such movement—due tooutput shaft 110's direct or indirect connection to the fins of themissile—likewise causes movement of the missile's fins and causes themissile to fly in an appropriate manner.

At a second side of body 112, projection 116 may be included and in somecases projection 116 may have a detent 118. Detent 118 is used to engagewith a portion of actuation mechanism 10′ to either allow movement ofoutput shaft 110 or lock output shaft 110 in a substantiallyimmovable/non-rotatable position. Such operation is set forth more fullybelow, after the differences between actuation mechanisms 10, 10′ aredescribed.

The differences between actuation mechanisms 10, 10′ are as follows. Asshown in FIGS. 3A-B, a portion of mounting 122 is equivalent to fixedhousing 20 from the previous embodiment—here referred to as fixedhousing 20′. Fixed housing 20′ is different from fixed housing 20 of theprevious embodiment in so far as it is monolithic with mounting 122, butalso because fixed housing 20′ does not include a groove 24 for aspring. Instead, fixed housing 20′ includes a hollow shaft 26′ and aflange or stepped area 123, with spring 27′ situated about hollow shaft26′ so as to abut flange 123. In the same way as the previousembodiment, actuation mechanism 10′ includes a plunger 40′ with a flange42′ that sandwiches spring 27′ between flange 42′ and flange 123 so thatactuation mechanism 10′ can operate in the same manner as actuationmechanism 10.

An additional difference between actuation mechanisms 10, 10′ is thatactuation mechanism 10′ includes an O-ring or other sealing member 126along its fixed housing 20′ to seal hollow shaft 26′. In this regard,fixed housing 20′ may include a tapered section for accommodating O-ring126, as shown in FIGS. 3A-B. Actuation mechanism 10′ also includes adifferent configuration of openings 80′ and set screws 82′ for itspiston 70′, and it includes a two-part piston 70′ wherein main body 74′of piston 70′ is separate from stepped shaft 76′. As shown in FIGS.3A-B, main body 74′ of piston 70′ includes a set of openings 80′ for setscrews 82′ that may function in the same manner as the previousembodiment—set screws 82′ act to fix wire 90′ to main body 74′.Alternatively, a first set screw 82′ may fix wire 90′ to main body 74′,while a second set screw 82′ can be used to connect a lead wire for theelectrical hook up to shape memory alloy wire 90′.

Main body 74′ is separate from stepped shaft 76′ and is positionedoutboard of flange 42′ of plunger 40′. In this regard, main body 74′ issomewhat larger in diameter than hollow shaft 44′ of plunger 40′ andabuts flange 42′ thereof. As shown, main body 74′ and stepped shaft 76′both still include internal channels 78′ for receiving wire 90′, muchlike above. Stepped shaft 76′ is positioned inside hollow shaft 44′ ofplunger 40′ and is configured to move from a locked position, as shownin FIG. 3A, to an unlocked position, as shown in FIG. 3B. Stepped shaft76′ may include its own mechanism for fixing wire 90′ to stepped shaft76′ (e.g., an opening 80′ and set screw 82′ that functions to securewire 90′ to stepped shaft 76′) so that, once wire 90′ is actuated via anelectric current or other stimulus, wire 90′ shortens in length andcauses stepped shaft 76′ to move in a laterally-rightward direction whenlooking to FIG. 3A. This movement, as with actuation mechanism 10, thencauses balls 56′ to move out of recesses 28′ and up against shaft 76′ sothat actuation mechanism 10′ is unlocked. Spring 27′ then acts againstflange 42′ of plunger 40′ to cause plunger 40′ to move outward away fromfixed housing 20′, in the same manner as actuation mechanism 10 setforth above.

When spring 27′ causes plunger 40′ to move outward and away from fixedhousing 20′, plunger 40′ consequently also moves out of engagement withdetent 118 in output shaft 110. This is shown in the progression betweenFIGS. 3A-B where it can be seen that plunger 40′ moves out of the way ofdetent 118 of output shaft 110 so that output shaft 110 is free torotate within mounting 122. In this manner, rotation of output shaft 110can then be controlled by the on-board computer and associated gearmechanism (not shown) for the missile to operate the missile's fins, andthus its flight.

An alternate reset mechanism is also provided for actuation mechanism10′. As shown in FIG. 2, the reset mechanism constitutes a bolt 142having a set of projections 146 that contact flange 42′ of plunger 40′.A set of arms 148 having openings 150 therein extend from mounting 122and are sized to receive bolt 142 and allow bolt 142 to rotate withinopenings 150 (allowing rotation of projections 146 as well). In anembodiment, pins 152 are also provided and extend through arms 148 toretain bolt 142 in arms 148. Bolt 142 additionally includes a drivemechanism 144 (e.g., a hexagonal recess) for engagement with a tool (notshown) to rotate bolt 142 and projections 146 thereof.

To reset actuation mechanism 10′, the tool (not shown) can be engagedwith drive mechanism 144 and rotated to rotate bolt 142 in acounterclockwise direction. This rotation causes projections 146 tocontact flange 42′ of plunger 40′ and move plunger 40′ in a rightwarddirection when looking to FIGS. 3A-B. Consequently, plunger 40′ may bemoved rightward until actuation mechanism 10′ is placed back into itslocked state, as shown in FIG. 3A. The locked state for actuationmechanism 10′ is the same as that for actuation mechanism 10, describedabove.

In the devices depicted in the figures, particular structures are shownthat are adapted for use in an actuation mechanism and/or a missile. Theuse of alternative structures for such purposes, including structureshaving different lengths, shapes, and configurations is alsocontemplated. As an example, although in certain cases threadedmechanisms are used herein, other connection mechanisms can also beused, such as bayonetted connections, press-fit (e.g., interference fit)connections, camming connections, etc. In addition, it should beappreciated that actuation mechanisms 10, 10′ can be used in multiplesub-assemblies for a missile to control the flight/fins thereof,although only one sub-assembly is described above. Further, other usesfor actuation mechanisms 10, 10′ are possible, including but not limitedto replacing solenoid actuators on inflation valves. Inflation valvesare typically one-time-use devices that use a solenoid to release abayonet, which punctures a burst disk to then allow high pressure gas toescape from its pressurized cylinder. The high pressure gas can be usedto do work, such as inflate a life raft, move an object, deploy a wing,etc. The actuation mechanisms 10, 10′ herein are usable as a replacementto the solenoid actuator for the aforementioned inflation valves.

In addition, although springs are used in various instances in actuationmechanisms 10, 10′, it is to be understood that other biasing membersmay be used as a substitute. For example, a compressible cylindricaldisc may be used. Other locking mechanisms beyond balls 56, 56′ may alsobe used, such as cylindrical rollers or round or square wire ringsegments.

As another example, although the reset mechanism described above inconnection with FIG. 2 is in the form of a bolt 142, any reset mechanismcan be used that causes flange 42, 42′ to move in a rightward direction,compressing spring 27, 27′ and causing locking balls 56, 56′ to moveback into their locked position. For instance, a motor might be providedwhich is actuated via a wireless signal (e.g., an RF signal transmittedto a receiver associated with the motor). The motor could have a movablestructure contacting flange 42, 42′ and causing it to move in arightward direction in response to the wireless signal.

Although aspects of the invention herein have been described withreference to particular embodiments, it is to be understood that theseembodiments are merely illustrative of certain features of the presentinvention. It is therefore to be understood that numerous modificationsmay be made to the illustrative embodiments and that other arrangementsmay be devised without departing from the spirit and scope of thepresent invention as defined by the appended claims. For instance, thefeatures described in connection with individual embodiments may beshared with others of the described embodiments.

It will also be appreciated that the various dependent claims and thefeatures set forth therein can be combined in different ways thanpresented in the initial claims. In particular, each feature from thedependent claims may be shared with other features of other claims, tothe extent technologically feasible, as if the claims were written inmultiple dependent format.

1. A method of operating an actuation mechanism comprising: positioninga plunger inside a bore in a housing, such that the plunger is lockedrelative to the housing; fixedly engaging a wire to a piston and to theplunger; and subjecting the wire to a stimulus so that the wire changesits length and causes the piston to move from a first position to asecond position, the movement of the piston from the first position tothe second position serving to unlock the plunger relative to thehousing so that the plunger is free to move inside the bore relative tothe housing.
 2. A method of operating an actuation mechanism as claimedin claim 1, wherein the stimulus is an electric current, a temperaturestimulus, or a combination thereof.
 3. A method of operating anactuation mechanism as claimed in claim 1, further comprising moving thepiston inside a bore in the plunger from its first position to itssecond position.
 4. A method of operating an actuation mechanism asclaimed in claim 1, wherein the wire is composed of a material selectedfrom the group consisting of a shape-memory alloy and a nickel-titaniumshape memory allow.
 5. A method of operating an actuation mechanism asclaimed in claim 1, further comprising moving the plunger relative tothe housing when unlocked.
 6. A method of operating an actuationmechanism as claimed in claim 5, further comprising causing an outputshaft associated with a missile sub-assembly to move after the plungerand housing are unlocked, the output shaft being coupled to a fin forcontrolling the flight of the missile.
 7. A method of operating anactuation mechanism as claimed in claim 5, further comprising expandinga spring engaged with the plunger and the housing to move the plungerrelative to the housing.
 8. A method of operating an actuation mechanismas claimed in claim 1, further comprising moving the piston from itsfirst position to its second position against the force of a springpositioned inside the plunger.
 9. A method of operating an actuationmechanism as claimed in claim 1, wherein the piston has at least oneinternal channel and the wire extends through the at least one internalchannel.